System and Method for Control of an Aircraft Cabin Display

1. A method for controlling an aircraft cabin display, the method comprising: measuring a reflected color on a surface adjacent to a cabin window of an aircraft that allows passage of light and through which a passenger may see outside of the aircraft; generating an image having an image color in accordance with the reflected color as measured on the surface adjacent to the cabin window; and displaying the image having the image color on a display device covering the cabin window to visually blend the window with the surface adjacent to the window, wherein: measuring the reflected color on the surface comprises measuring a first reflected color at a first position on the surface and measuring a second reflected color at a second position on the surface; generating the image comprises generating a first portion of the image in accordance with the first reflected color and generating a second portion of the image in accordance with the second reflected color; and a color gradient is applied across the first and second portions of the image displayed on the display device.

2. The method of claim 1 , further comprising obtaining a reflected intensity of light at the surface adjacent to the cabin window, and wherein generating an image comprises generating the image with an image intensity in accordance with the reflected intensity.

3. The method of claim 1 , wherein the first position and the second position on the surface adjacent to the cabin window are on opposite sides of the cabin window.

4. The method of claim 1 , wherein the display extends over the cabin window and a plurality of additional cabin windows adjacent to the cabin window, and wherein displaying the image comprises displaying the image on a portion of the display covering the cabin window.

5. The method of claim 4 , further comprising measuring additional reflected colors on respective surfaces adjacent to the plurality of additional cabin windows, generating respective additional images in accordance with the additional reflected colors as measured, and displaying the additional images on respective portions of the display covering the additional cabin windows.

6. The method of claim 5 , wherein the plurality of additional cabin windows are separated by cabin wall sections, and further comprising rendering the display transparent over portions of the display corresponding to the cabin wall sections.

7. The method of claim 1 , further comprising enabling the displaying of the image upon detection of a predetermined level of translucency of the cabin window.

8. The method of claim 1 , wherein the method is applied dynamically as lighting conditions inside the aircraft cabin change.

9. A system for controlling an aircraft cabin display, the system comprising: a processing unit; and a non-transitory computer-readable medium having stored thereon program code executable by the processing unit for: measuring a reflected color on a surface adjacent to a cabin window of an aircraft that allows passage of light and through which a passenger may see outside of the aircraft; generating an image having an image color in accordance with the reflected color as measured on the surface adjacent to the cabin window; and displaying the image having the image color on a display device covering the cabin window to visually blend the window with the surface adjacent to the window; wherein: measuring the reflected color on the surface comprises measuring a first reflected color at a first position on the surface and measuring a second reflected color at a second position on the surface; generating the image comprises generating a first portion of the image in accordance with the first reflected color and generating a second portion of the image in accordance with the second reflected color; and a color gradient is applied across the first and second portions of the image displayed on the display device.

10. The system of claim 9 , wherein the program code is further executable for obtaining a reflected intensity of light at the surface adjacent to the cabin window, and wherein generating an image comprises generating the image with an image intensity in accordance with the reflected intensity.

11. The system of claim 9 , wherein the first position and the second position on the surface adjacent to the cabin window are on opposite sides of the cabin window.

12. The system of claim 9 , wherein the display extends over the cabin window and a plurality of additional cabin windows adjacent to the cabin window, and wherein displaying the image comprises displaying the image on a portion of the display covering the cabin window.

13. The system of claim 12 , wherein the program code is further executable for measuring additional reflected colors on respective surfaces adjacent to the plurality of additional cabin windows, generating respective additional images in accordance with the additional reflected colors as measured, and displaying the additional images on respective portions of the display covering the additional cabin windows.

14. The system of claim 13 , wherein the plurality of additional cabin windows are separated by cabin wall sections, and further comprising rendering the display transparent over portions of the display corresponding to the cabin wall sections.

15. The system of claim 9 , wherein the program code is further executable for enabling the displaying of the image upon detection of a predetermined level of translucency of the cabin window.